Design and Simulation of an Improved Five Redundancy GNC System Architecture
2014 ◽
Vol 543-547
◽
pp. 1423-1427
Keyword(s):
Data Bus
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Aerospace plane, the next generation manned spacecraft has the characteristics of high reliability and high security. Therefore, a five modular redundancy byzantine fault tolerant architecture is propose for the guidance, navigation and control (GNC) system. This architecture can give the system characteristic of double fault resilience, and is also suitable for solving Byzantine general problem. A semi-physical simulation is done, which is based on 1553B data bus and VxWorks operating system. The simulation result has verified the fault tolerant architecture and feasibility of the system implementation.
Keyword(s):
2020 ◽
Vol 35
(1)
◽
pp. 51-67
2014 ◽
Vol 573
◽
pp. 209-214
2010 ◽
Vol 17
(04)
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pp. 331-350
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2017 ◽
Vol 8
(1)
◽
pp. 3-7
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1990 ◽
Vol 38
(433)
◽
pp. 60-65